发明名称 HIGH TEMPERATURE SPEED SENSOR
摘要 A gas turbine shaft speed sensor including a sensing coil comprised of a central conducting wire, the sensor and conducting wire is surrounded by a layer of mineral insulator and the mineral insulator is surrounded by a metallic, non magnetic, sheath. A sensing coil formed with this construction allows th e high operating temperatures and is robust.
申请公布号 CA2667862(A1) 申请公布日期 2009.12.06
申请号 CA20092667862 申请日期 2009.06.01
申请人 WESTON AEROSPACE LIMITED 发明人 TURNER, NIGEL PHILIP
分类号 G01P3/44;F01D25/00;G01P3/49 主分类号 G01P3/44
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